Debris dispersion effect in N-shape configuration☆
作者： Xue-zhong Wen , Jie Huang , Fa-wei Ke , Zhao-xia Ma , Sen Liu
DOI: 10.1016/J.ACTAASTRO.2014.06.037
关键词:
摘要: Abstract Spacecraft shields play an important role in shielding against the impact of space debris. Increasing dispersion degree debris produced by on bumper configuration is able to lower concentration impacting rear plate and thus reduce risk perforating plate. In order improve degree, N-shape proposed studied hypervelocity test with velocity 4.80 km/s numerical simulation velocities ranging from 3.0 km/s 7.0 km/s. As a comparison, distribution also investigated for parallel triple-wall same areal density. It found that this increased due oblique plate, therefore reduced compared case configuration.
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